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Analysis on three-dimensional flow and heat transfer in a cross wavy primary surface recuperator for a microturbine system

机译:微型涡轮系统横波一次表面换热器中的三维流动和传热分析

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In this paper, three-dimensional periodic numerical model for fully developed flow in a cross wavy primary surface recuperator for a microturbine system is built. The performance of flow and heat transfer is analyzed. The fields of flow and temperature in a gas and air channel are obtained. Different working conditions are numerically simulated. Numerical results are compared with experimental data concerned. Analysis results show that the flow in the gas and air channel is anti-symmetry along the centre of channel. The flow of fluid is fluctuant. The flow velocity of gas is much higher than that of air. The thermal ratio of cross wavy primary surface recuperator can reach 95.2%. The thermal ratio decreases with the improvement of gas inlet temperature. When gas inlet temperature increases by 100 K, the thermal ratio decreases by about 1%. The thermal ratio increases with the reduction of flow rate in the channel. When flow rate reduces by 40%, the thermal ratio increases by about 4%. The research results can be used to guide checking the performance of a recuperator.
机译:在本文中,建立了用于微涡轮系统的交叉波浪形主表面同流换热器中充分发展的流动的三维周期数值模型。分析了流动和热传递的性能。获得了气体和空气通道中的流量和温度场。数值模拟了不同的工作条件。将数值结果与有关的实验数据进行比较。分析结果表明,气体和空气通道中的流动沿通道的中心是反对称的。流体的流量是波动的。气体的流速远高于空气的流速。波浪形初级表面换热器的热效率可达95.2%。随着进气温度的提高,热比降低。当气体入口温度增加100 K时,热比降低约1%。热比随着通道中流速的降低而增加。当流量减少40%时,热比增加约4%。研究结果可用于指导检查同流换热器的性能。

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